Relevant bibliographies by topics / Metal-reinforced laminate

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Book chapters
  4. Conference papers

Academic literature on the topic 'Metal-reinforced laminate'

Author: Grafiati
Published: 5 June 2025
Last updated: 24 June 2025

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Journal articles on the topic "Metal-reinforced laminate"

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Stoll, Matthias, Franziska Stemmer, Sergej Ilinzeer, and Kay André Weidenmann. "Optimization of Corrosive Properties of Carbon Fiber Reinforced Aluminum Laminates due to Integration of an Elastomer Interlayer." Key Engineering Materials 742 (July 2017): 287–93. http://dx.doi.org/10.4028/www.scientific.net/kem.742.287.

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Fiber-Metal-Laminates (FML) show superior dynamic mechanical properties combined with low densities. The mechanical performance of for example commercially available fiber-metal-laminate, glass laminate aluminum reinforced epoxy, can be improved by the substitution of glass fibers with carbon fibers. However, carbon fiber reinforced aluminum laminate introduces a mismatch of coefficients of thermal expansion and the possibility of galvanic corrosion. The fiber-metal-laminate is altered by the integration of an elastomer interlayer which is desired to solve both problems. The high electrical resistance is supposed to inhibit the corrosion. This study focuses on the effect of galvanic corrosion caused by neutral salt spray tests on fiber-metal-laminates, the influence of an elastomer interlayer and the quantification of the residual mechanical properties. The galvanic corrosion affects the interfaces of the laminates, therefore in this study edge shear tests and flexural tests were carried out to quantify the residual properties and thereby the corrosive damage. The elastomer interlayer was found to inhibit galvanic corrosion in the salt spray chamber, whereas the fiber-metal-laminate without interlayer showed corrosive damage. Furthermore, the mechanical properties of the fiber-metal-laminate with elastomer interlayer remained constant after the corrosion tests, whilst the fiber-metal-laminate’s properties decreased with corrosive loads.
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Salve, Aniket, Ratnakar Kulkarni, and Ashok Mache. "A Review: Fiber Metal Laminates (FML’s) - Manufacturing, Test methods and Numerical modeling." International Journal of Engineering Technology and Sciences 3, no. 2 (2016): 71–84. http://dx.doi.org/10.15282/ijets.6.2016.1.10.1060.

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Weight reduction of components is the main aim of different industrial sectors. This leads to increasing application areas of fiber composites for primary structural components. Aiming this objective, a new lightweight Fiber/Metal Laminate (FML) has been developed. Fiber metal laminate is one such material which is being widely investigated for its performance compared to existing material.. The most commercially available fiber metal laminates (FML’s) are ARALL (Aramid Reinforced Aluminium Laminate), based on aramid fibers, GLARE (Glass Reinforced Aluminium Laminate), based on high strength glass fibers and CARALL (Carbon Reinforced Aluminium Laminate), based on carbon fibers. The mechanical properties of FML show advantages over the properties of both aluminium alloys and composite materials individual. This paper reviews relevant literature which deals with different manufacturing techniques for FML’s with excellent properties under tensile, flexure and impact conditions. It also reviewed recent modeling techniques on FML’s. Modeling of tensile, flexure and impacts behavior on fiber metal laminates requires understanding the bonding between the metal and composite layer. Further research is necessary in the assessment of mechanical performance of complex structures in real world conditions.
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Lu, Hongbin, Dongfa Sheng, Yuting Fang, Hongquan Yu, and Fan Yang. "Analysis of Tensile Failure Behavior of Metal Fiber Laminates Under Different Temperature Environments." Polymers 16, no. 23 (2024): 3319. http://dx.doi.org/10.3390/polym16233319.

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The tensile properties of fiber metal laminates were examined at temperatures ranging from 30 °C to 180 °C in this paper through the integration of numerical simulation techniques, experimental measurements, and digital image correlation techniques. The laminates were initially modeled using finite elements, and the failure behavior of porous basalt-fiber-reinforced aluminum alloy plates was numerically simulated. Consequently, metal fiber laminate stress–strain responses were varied by numerous tensile experiments conducted at varying temperatures. Simultaneously, a scanning electron microscope was used to scan a porous basalt-fiber-reinforced aluminum alloy laminate at different temperatures to determine the tensile mechanical behavior and micro-damage morphology. Lastly, the laminate’s dynamic response to the tensile process was observed through digital image correlation technology. The stress distribution was determined to be concentrated around circular openings through analysis. The strain distribution graph exhibited a “band” shape as the number of perforations increased. The findings indicate that fiber metal laminates lose tensile strength as temperatures increase. The ultimate tensile strength of the laminate decreases as the number of perforations increases at the same temperature. Complex damage mechanisms, including matrix debonding, fiber withdrawal, and matrix fracture, can be captured through scanning electron microscopy at varying temperatures. The tensile behavior and damage mechanisms of laminates with hole-containing structures under thermal conditions are examined, and the results can be used to inform the design and utilization of laminate structures.
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Frankiewicz, Mariusz, Grzegorz Ziółkowski, Robert Dziedzic, Tomasz Osiecki, and Peter Scholz. "Damage to inverse hybrid laminate structures: an analysis of shear strength test." Materials Science-Poland 40, no. 1 (2022): 130–44. http://dx.doi.org/10.2478/msp-2022-0016.

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Abstract Hybrid laminates with continuous fiber reinforcement, such as glass reinforced aluminium laminate (GLARE), aramid reinforced aluminum laminate (ARALL), or carbon reinforced aluminum laminate (CARALL), have been developed to increase the lightweight potential and fatigue resistance applied for aircraft structures. However, the use of thermosetting matrices imposes material limitations regarding recycling, malleability, and manufacturing-cycle times. The inverse hybrid laminate approach is based on a continuous fiber-reinforced thermoplastic matrix, in which a metal insert is integrated. For efficient manufacturing of the novel composites in high-volume production processes, conventional sheet metal–forming methods have been applied. It helped to reduce the cycle times and the costs of the forming equipment compared to currently used hybrid laminate-processing technologies. The present study analyzes the damage to the inverse hybrid laminate structures resulting from the interlaminar shear strength test. The tests were performed for eight laminate material configurations, which differed by the type and directions of the reinforced glass and carbon fibers in the polyamide matrix and the number of the fiber-reinforced polymer (FRP) layers in the laminates. Industrial computed tomography and scanning electron microscopy were used for analysis. Observed damages, including fiber–matrix debonding, fiber breakages, matrix fractures, interfacial debonding, and delamination in selected areas of the material, are strictly dependent on the laminate configurations. FRP layers reinforced by fibers perpendicular to the bending axis presented better resistance against fractures of the matrix, but their adhesion to the aluminum inserts was lower than in layers reinforced by fibers parallel to the bending axis.
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Vilas Boas, Cristiane, Felipe Moreno, and Demetrio Jackson dos Santos. "Mechanical Analysis of Polybenzoxazine Matrix in Fiber Metal Laminates." Materials Science Forum 869 (August 2016): 215–20. http://dx.doi.org/10.4028/www.scientific.net/msf.869.215.

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In this work we investigated the application of a novel high performance polymer, polybenzoxazine, as a polymeric matrix in Fiber Metal Laminates (FML). This polymer, when applied on the development of FMLs, generated higher mechanical properties in comparison to fiber metal laminates obtained with epoxy. To investigate the mechanical performance of the polybenzoxazine matrix in FMLs, a mechanical behavior comparison was carried out among epoxy matrix laminates - glass fiber reinforced aluminum laminate (GLARE) and carbon fiber reinforced aluminum laminate (CARALL) - and FML constructed with aluminum and carbon fiber reinforced polybenzoxazine. The mechanical properties were characterized by drop weight impact and flexural methods, and the polybenzoxazine curing behavior through differential scanning calorimetry (DSC). Polybenzoxazine FML generated increasing of: 18% of maximum load, 11% of maximum elongation under flexure and 7.5% of impact energy absorption compared to other fiber metal laminates.
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Neugebauer, Reimund, Verena Kräusel, and Alexander Graf. "Process Chains for Fibre Metal Laminates." Advanced Materials Research 1018 (September 2014): 285–92. http://dx.doi.org/10.4028/www.scientific.net/amr.1018.285.

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The combination of fibre-reinforced materials with metals is defined as a fibre metal laminate. These material composites have already been a subject of research for several years. The long manufacturing time resulting from the period required for consolidation of the thermosetting resin is a major disadvantage of the fibre metal laminates previously in use (for instance GLARE, which is a combination of aluminium with glass fibre-reinforced plastic). In this paper, a new fibre metal laminate with a thermoplastic resin in the carbon fibre-reinforced plastics (CFRP) is introduced. The application of a thermoplastic resin system results in a general change in the process chain. The cutting of fibre metal laminates by means of the flexible water jet and laser cutting techniques is presented. In the second operation, forming behaviour is represented by the methods of v-bending and deep drawing. Finally, quality assurance by means of computed tomography, which replaces the conventional metallographic method, is described.
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Xie, Botao, Liang Gao, Shuai Jiang, Shangda Zhang, Chen Wu, and Xu Ran. "Notched tensile response and damage mechanism of the GLARE laminate." Journal of Composite Materials 54, no. 22 (2020): 3037–46. http://dx.doi.org/10.1177/0021998320907963.

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Glass laminate aluminum reinforced epoxy, as an attractive material for advanced aerospace applications, is most likely to face the challenge of various blunt notched damages. In this paper, the tensile tests of the glass laminate aluminum reinforced epoxy with circular and square blunt notches are conducted. The effects of notch geometry, such as notch diameter, notch corner radius, and off-axis angle, on the laminated tensile behaviors of glass laminate aluminum reinforced epoxy laminate are explored. A characteristic distance function representing the damage-affected region of notch is empirically constructed to predict the residual strength of the circular notched glass laminate aluminum reinforced epoxy based on a modified point stress criterion. For the square notched laminate, the strength is almost equal to that of the laminate with its circumscribed circle notch. Furthermore, the variation of two fracture patterns observed with the notch geometry is studied, and the evolution of the interlaminar delamination damage is analyzed after the metal chemical removal.
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Feng, Ng Lin, Sivakumar DharMalingam, Kamarul Ariffin Zakaria, and Mohd Zulkefli Selamat. "Investigation on the fatigue life characteristic of kenaf/glass woven-ply reinforced metal sandwich materials." Journal of Sandwich Structures & Materials 21, no. 7 (2017): 2440–55. http://dx.doi.org/10.1177/1099636217729910.

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Fatigue life characteristic of hybrid composite reinforced metal laminate is a notable investigation since this kind of material offers several superior characteristics over conventional metallic alloy. A majority of the researches have focused on the mechanical properties of hybrid composite and conventional fibre metal laminate such as glass reinforced aluminium epoxy and aramid fibre reinforced aluminium laminate. However, investigation on the fatigue life behaviour of hybrid composite reinforced metal laminate still remains unexplored. In this study, the fatigue life characteristic of hybrid kenaf/glass reinforced metal laminate with different fibre configurations, orientation and stress ratio was presented. Fibre metal laminate was manufactured through hot press moulding compression method using annealed aluminium 5052 as the skin layers and the composite laminate as the core constituent. Tensile test was conducted at a quasi-static rate in accordance with ASTM E8 while tension–tension fatigue test was conducted at force controlled constant amplitude according to ASTM E466. Experimental results revealed that fibre metal laminate with 0°/90° fibre orientation exhibited better tensile and fatigue properties compared to fibre metal laminate with ±45° fibre orientation regardless of the woven-ply fibre configurations. Besides that, it was identified that higher stress ratio improves the fatigue life cycle of the fibre metal laminate structures.
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Yeoh, T. S., S. Saadon, and N. Mazlan. "Fire properties test on fibre metal laminate based on carbon/flax fibre composites reinforced with silicon carbide for aircraft engine fire-designated zones." IOP Conference Series: Earth and Environmental Science 1500, no. 1 (2025): 012043. https://doi.org/10.1088/1755-1315/1500/1/012043.

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Abstract Due to the problems of flammability, weight and health risk associated with the materials in the fire designated zone of an aircraft engine, there is a need to develop new composites that will resolve the fire issues. Accordingly, new composites, the fibre metal laminates reinforced silicon carbide will be examined in this research. The fibre metal laminate composites using carbon/flax fibre will be tested with aluminium alloy. The study presents a novelty in hybridising the synthetic/natural fibre with nanocomposites in the fire designated zone of an aircraft engine. To ensure the validity of such composites, the fire resistance, and thermal properties of the materials were experimentally investigated in this research. Four laminates with different compositions were fabricated using the hand lay-up method: Carbon Fibre Reinforced Aluminium Alloy Laminate (CARALL), Carbon/Flax Fibre Reinforced Aluminium Alloy Laminate (CFFRAL) and one of each laminate with the inclusion of silicon carbide (SiC) nanoparticles as fillers. The main aim of the study is to investigate the fire operational performance of the fabricated composites for the fire designated zone of an aircraft engine at some high temperature for future use in aerospace industries. The composites’ different layers, stacking sequence, and materials with the same thickness will be fabricated in a mould using the hand lay-up method. The burn-through fire test will be carried out using a standardised burner. The results of the fire test on all the four laminates show that all the laminates are fireproof and although the laminates contain less than 37.5% of carbon fibre, it is still able to achieve nearly the same results as fully carbon fibre metal laminate.
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Trautmann, Maik, Selim Mrzljak, Frank Walther, and Guntram Wagner. "Mechanical Properties of Thermoplastic-Based Hybrid Laminates with Regard to Layer Structure and Metal Volume Content." Metals 10, no. 11 (2020): 1430. http://dx.doi.org/10.3390/met10111430.

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Multi layered lightweight material compounds such as hybrid laminates are composed of different layers of materials like metals and unidirectional fibre-reinforced plastics and offer high specific strength. They can be individually tailored for applications like outer cover panels for aircraft and vehicles. Many characteristics especially layer structure, volume contents of the embedded materials as well as layer surface adhesion determine the performance of a hybrid laminate. In this study, the influence of layer structure and metal volume content are evaluated with regard to the mechanical properties of the recyclable hybrid laminate CAPAAL (carbon fibre-reinforced plastics/aluminium foil laminate), which consists of the aluminium alloy AA6082 and a graded structure of glass and carbon fibre-reinforced polyamide 6. Hybrid laminates with different ratios of the fibre-reinforced plastic and numbers of aluminium layers were manufactured by thermal pressing. The consolidation quality of in total four laminate structure variations, including 2/1 and 3/2 metal-to-fibre-reinforced plastic layer structures with fibre orientation variation, were investigated by light microscopy through cross-sections and further on computed tomography. For determination and evaluation of the mechanical properties metrologically instrumented quasi-static tensile and three-point bending tests, as well as tension-tension fatigue tests for the establishment of S-N curves were performed. The results were correlated to the microstructural observations, revealing significant influence by the consolidation quality. The layer structure proved to have a proportional impact on the increase of quasi-static tensile and flexure strength with a decrease in metal volume content. Orienting some of the fibre-reinforced plastic layers in ±45° leads to a more evenly distributed fibre alignment, which results in a higher consolidation quality and less anisotropic bending properties. Fatigue results showed a more complex behaviour where not only the metal volume content seems to determine the fatigue loading capability, but also the number of metal-fibre-reinforced plastic interfaces, hinting at the importance of stress distribution between layers and its longevity over fatigue life.
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Dissertations / Theses on the topic "Metal-reinforced laminate"

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Guzmán, J. Fernando Guillén. "Cooling rate effects in glass reinforced thermoplastic-based fibre metal laminates." Thesis, University of Liverpool, 2002. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.399210.

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Macháčková, Eva. "Vícepodlažní dřevostavba." Master's thesis, Vysoké učení technické v Brně. Fakulta stavební, 2013. http://www.nusl.cz/ntk/nusl-226117.

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Master’s thesis deals with complete project documentation of newly built object of library and mediatheque located on the site in České Budějovice. It is a three-storey building divided into three parts, one-storey, two-storey and three-storey. It is partly basement. The underground part is devoted to main storage spaces of library services, management offices and social facilities for staff (toilets, changing rooms, washrooms). This part of the building has own entrance for employees. In the 1st floor is located the main library area along with exhibition spaces and the main entrance for visitors with self service cloakroom. In the 2nd floor are designed library spaces for visually impaired persons with fund of audio books, CDs and DVDs, a lecture hall with a projector and own kitchen and space for reading magazines and periodicals. From this floor is possible access to the outdoor terrace, which has own terrace furniture store nearby. In the 3rd floor is located a literary café with its own facilities. In each floor are also designed sanitary facilities for use by persons with limited ability of movement and orientation. All floors are connected by stairs and passenger lifts. In terms of construction, the building is designed as a frame, in the underground parts made of reinforced concrete, the overhead of glued laminated timber elements. The ceiling structure designed over the underground floor is monolithic reinforced concrete slab. The ceilings in the upper part are designed as a wooden beamed made of the glued laminated timber elements. The building has a pent roof created by wooden trusses assembled with punched metal plate fasteners. The foundations are designed as belts and footings. The study, detailed documentation, thermal-technical evaluation of selected structures and fire safety of the building are processed. For processing of the thesis were used software AutoCAD 2010, Teplo 2011, Area 2011, Ztráty 2011 and Fire NX 802 PRO.
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Nam, Jae. "Deformation and Failure Behaviour of Self-reinforced Polypropylene and Self-reinforced Polypropylene/Steel Fibre Metal Laminate." Phd thesis, 2020. http://hdl.handle.net/1885/206296.

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This thesis discusses material behaviours related to the failure of woven self-reinforced polypropylene (SRPP) and a fibre metal laminate (FML) based on SRPP and mild steel. Single polymer composites such as SRPP are relatively new, as compared to the traditional fibre-reinforced composites, and while there have been studies that investigate the optimal manufacturing methods, there are relatively few that look at the failure behaviour of SRPP in depth. On top of this, SRPP exhibits behaviours that are quite different from most traditional fibre-reinforced polymers due to its unique construction. As a result, there is also limited knowledge of the behaviour of SRPP-based FMLs, except under impact. A better understanding of these materials will be valuable, given that they have a lot of potential uses in many applications, especially for those that can benefit from recyclability, high impact resistance and weight reduction. For this reason, failure, and related deformation behaviours of SRPP and SRPP/steel FML, were investigated. The material behaviours were studied using different reinforcing directions under uniaxial tension, and different specimen geometries under combined in-plane biaxial and out-of-plane bending deformations, for both the SRPP and FML. In addition, specimens of different thicknesses were studied for SRPP under uniaxial tension, which behave differently and give important insights into the failure mechanisms. Analyses were carried out using a combination of microscopy and surface strain analysis, which can effectively be used to study various damage types in SRPP and their relation to the failure of SRPP and FML. In this research, various types of damage and related mechanisms were uncovered, some of which have not been previously reported in the literature. One of the most important aspects was that the critical damage mechanisms that cause failure in the materials were identified for different material and loading conditions. This includes a particular type of matrix damage in SRPP which was found to cause an unusually high strain concentration and, as a result, lead to material failure in some cases. It was found that failure from such damage can be suppressed in some specimens which exhibit mechanisms that can impede damage growth. It was found that the process of damage development, and how this relates to the failure behaviour, can depend on one or more of the following factors, some of which are related: damage type, presence (or lack) of toughening mechanisms, mode of crack propagation, reinforcing direction, weave geometry, sensitivity to local damage, loading condition, material thickness, and consolidation quality. Some of these factors can influence the failure behaviour to the point that the same type of specimen, subjected to the same loading condition, can fail from different regions of the material, under different failure mechanisms. In the course of the analysis, it was found that, in many cases, the surface strains captured during the deformation process can indicate where, and under which conditions, failure occurred. The findings from this research highlighted the importance of understanding the exact mechanisms behind the failure of SRPP, SRPP-based FML and similar materials, since they can vary significantly depending on numerous factors. It is anticipated that the findings from this study will lay the groundwork for future research on developing failure criteria for such material systems for the benefit of researchers and designers using composite and hybrid materials.
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Book chapters on the topic "Metal-reinforced laminate"

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Jia, Zehui, Lingwei Xu, Shuangkai Huang, Haoran Xu, Zhimo Zhang, and Xu Cui. "Preparation and Impact Resistance of Carbon Fiber Reinforced Metal Laminates Modified by Carbon Nanotubes." In Lecture Notes in Civil Engineering. Springer Singapore, 2022. http://dx.doi.org/10.1007/978-981-19-1260-3_27.

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AbstractFiber reinforced metal laminates (FMLs) are a kind of interlaminar hybrid composites made of metal sheets and fibers alternately stacked and cured at a certain pressure and temperature. In this paper, through the simulation of ABAQUS finite element software and recording the change of projectile velocity, the energy loss of projectile is calculated and the impact resistance is judged. Through the comparison of three groups of simulation experimental results, the energy absorbed by carbon fiber reinforced metal laminate is about 300 times that of aluminum alloy plate, which fully shows that carbon fiber reinforced metal composite has excellent impact resistance compared with aluminum alloy. After adding 1 wt% carbon nanotubes to carbon fiber reinforced metal laminates, the absorbed energy is about 10 times that of the original, which shows that carbon nanotubes improve the ultimate yield stress of resin and materials in epoxy resin and enhance the weakness that the composites are easy to delamination under impact load.
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Sun, Chen, Minghua Dai, Liang Ying, Kai Du, Zhigang Chen, and Ping Hu. "Experimental and Numerical Simulation on Formability and Failure Behavior of Thermoplastic Carbon Fiber/AL Composite Laminates." In Lecture Notes in Mechanical Engineering. Springer International Publishing, 2024. http://dx.doi.org/10.1007/978-3-031-58006-2_30.

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AbstractCarbon fiber reinforced thermoplastic/aluminum alloy (CFRTP/AL) composite laminates have the advantages of low density, high specific strength, and good fatigue resistance, which is a new type of engineering composite material to realize lightweight vehicle body. Heterogeneous interface delamination failure occurs in the forming process of the fiber metal laminates (FMLs). It is necessary to establish an effective finite element simulation strategy to accurately predict the delamination failure behavior of FMLs. In this work, thermoplastic PA6 continuous carbon fiber/AL FMLs were taken as the research object, and the double cantilever beam (DCB) and the end-notched flexure (ENF) experiments were carried out to determine the basic mechanical parameters between the interlayer interfaces of CFRTP/AL. Furthermore, a numerical simulation model based on ABAQUS software was developed to describe the progressive damage failure behavior of the CRFTP/AL in the forming process by using the equivalent modeling strategy of discontinuous micro-shear, which realized the effective prediction of ply directional damage failure of FMLs on the basis of the S-beam model. The results show that the established damage constitutive model and numerical method coupled with cohesive zone model (CZM) can effectively predict the ply directional damage failure behavior of CFRTP/AL composites during the large deformation forming.
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Abdullah, M. R., and W. J. Cantwell. "The High Velocity Impact Response of Self-Reinforced Polypropylene Fibre Metal Laminates." In Advanced Structured Materials. Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-23659-4_13.

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Pidge, Abhijeet, Aniket Salve, Ashok Mache, Aparna Kulkarni, and Yashwant Munde. "Effect on Vibration Characteristics of Fiber Metal Laminates Reinforced with Jute/glass Fibers." In Advances in Engineering Materials. Springer Nature Singapore, 2023. http://dx.doi.org/10.1007/978-981-99-4758-4_11.

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Rolfes, Raimund, Christian Gerendt, and Martin Brod. "New Approaches for Progressive Damage Analysis of Fiber Reinforced Composites and Fiber Metal Laminates." In Current Trends and Open Problems in Computational Mechanics. Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-030-87312-7_44.

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Kim, Cheol Woong, Sam Hong Song, and Dong Joon Oh. "Proposal of Pseudo Crack Model for the Un-Cracking Delamination Behavior of Fiber Reinforced Metal Laminates." In Materials Science Forum. Trans Tech Publications Ltd., 2005. http://dx.doi.org/10.4028/0-87849-960-1.941.

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Kim, Cheol Woong, Sam Hong Song, Dong Joon Oh, and Kwang Joon Yoon. "Verification of the Delamination Growth Rate (dAD/da) in Fiber Reinforced Metal Laminates." In Key Engineering Materials. Trans Tech Publications Ltd., 2005. http://dx.doi.org/10.4028/0-87849-978-4.195.

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Logesh, K., V. K. Bupesh Raja, M. Venkatasudhahar, and Hitesh Kumar Rana. "Experimental Investigation on Tensile and Fracture Behaviour of Glass Fibre-Reinforced Nanoclay/Mg–Al LDH-Based Fibre Metal Laminates." In Lecture Notes in Mechanical Engineering. Springer Singapore, 2018. http://dx.doi.org/10.1007/978-981-13-2718-6_4.

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"Tensile Testing of Fiber-Reinforced Composites." In Tensile Testing, 2nd ed. ASM International, 2004. http://dx.doi.org/10.31399/asm.tb.tt2.t51060183.

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Abstract This chapter presents the fundamentals of tensile testing of fiber-reinforced polymer composites. Basic tensile testing of polymer composites is divided into lamina and laminate testing. The chapter focuses on tensile testing of laminates. It discusses the most common tensile test methods that have been standardized for fiber-reinforced composite materials. It also briefly reviews considerations in tensile testing of metal-matrix composites.
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Pablo Reis, Ruham, Iaroslav Skhabovskyi, Alberto Lima Santos, Leonardo Sanches, Edson Cocchieri Botelho, and Américo Scotti. "Fiber-Metal Laminate Panels Reinforced with Metal Pins." In Optimum Composite Structures. IntechOpen, 2019. http://dx.doi.org/10.5772/intechopen.78405.

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Conference papers on the topic "Metal-reinforced laminate"

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Baliashvili, Giorgi, Sophiko Kvinikadze, Tamar Iashvili, Davit Tsverava, and Aleksandre Vanishvili. "DEVELOPMENT OF METAL-POLYMER LAMINATE WITH HIGH MECHANICAL PROPERTIES." In SGEM International Multidisciplinary Scientific GeoConference 24. STEF92 Technology, 2024. https://doi.org/10.5593/sgem2024/6.1/s24.04.

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Basalt fiber-reinforced metal-polymer composites represent a cutting-edge class of materials that merge the robustness of metal with the pliability of polymer. Originating from natural volcanic rocks, basalt fibers possess remarkable mechanical properties, such as high tensile strength, resistance to extreme temperatures, and chemical inertness. Integrating basalt fibers into a polymer matrix like epoxy or thermoplastic resins significantly boosts the composite's resistance to dynamic impacts and its energy absorption capacity. The metal component ensures structural integrity and strength, while the polymer matrix distributes energy through elastic deformation. Basalt fibers find application across various industries, including aviation, automotive, and military technology. There are research centers and scientific groups whose work is focused on developing polymer composite materials reinforced with basalt fibers. These metal-polymer composites are especially valuable for their application in an automotive industry, aerospace and construction, due to their high strength to weight ratio, as well as for the ability to absorb impact energy, flexibility in design and chemical resistance. The objective of this study is to develop a technology for producing basalt fiber-based metal-polymer composites and to investigate the physical and mechanical properties of these materials. Using Vacuum Infusion Process (VIP) technology, metal-polymer composites incorporating basalt fiber were produced. The resulting samples exhibit high bonding strength, uniform polymer distribution within the matrix, and a straightforward manufacturing process. Experimental samples of the metal-polymer composites, produced using VIP technology, were tested under mechanical and dynamic loads.
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Reith, Hans-Juergen. "Dual Laminate Pipework and Vessels with a Bonded PTFE Lining Suitable for Corrosive Media at High Temperature." In CORROSION 2007. NACE International, 2007. https://doi.org/10.5006/c2007-07543.

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Abstract Components used in chemical plants are exposed to extreme stresses due to process conditions. Aggressive media, pressure differences and marked changes in temperature require corrosion protection systems combining high chemical resistance, good mechanical strength and high thermal stability to insure permanently reliable plant operation. Conventional metal equipment and pipe work systems often fail to meet expectations for lasting reliability. For many decades now, glass fiber-reinforced unsaturated polyester and vinylester resins (FRP) have been a familiar and highly appreciated alternative to metal materials. With their chemical-resistant layer and thermoplastic liner they offer good corrosion resistance and are thus ideal materials for equipment and pipe work construction. Up to the 1990s, the media usually handled and stored were aqueous liquids, so that materials with dimensional stability of up to 125°C were adequate. Since then, increasing use has been made of plastic components, especially in constructing equipment and plant components exposed to high thermal stresses in chemical process engineering. Consequently, the demand for higher thermal and chemical stability of the construction materials has increased as well. The product found to meet such demands is a composite system comprising a load-bearing FRP layer and, firmly bonded to it, a modified polytetrafluoroethylene liner. This paper outlines the development of this relatively new composite material. It also describes the practical experience the chemical process engineering industry has gained with this material. Such experience relates in particular to demanding applications combining both aggressive media and high temperatures.
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Sawant, Sourabh, and Anastasia Muliana. "A Nonlinear Viscoelastic Modeling of Fiber Metal Laminates." In ASME 2007 International Mechanical Engineering Congress and Exposition. ASMEDC, 2007. http://dx.doi.org/10.1115/imece2007-42152.

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A new class of advanced composite materials namely the fibermetal laminates (FMLs) such as ARALL (Aramid Reinforced Aluminum laminate) and GLARE (Glass Reinforced Aluminum laminate) has been developed for primary load bearing components of aircraft fuselage and wings. The FML is composed of alternating layers of fiber reinforced polymer (FRP) and aluminum sheets and shows good fatigue resistance. The metal layers are placed on the top and bottom of the laminate to provide good impact resistance and resistance to extreme environments (moisture, ultraviolet radiation and solvent). Krishnakumar (1994) has provided a survey of extensive works on manufacturing, testing, and modeling of the FMLs. The FMLs exhibit nonlinear viscoelastic and/or plastic behaviors due to the existence of FRP and metal alloy layers. The nonlinearity and time-dependent responses in the FMLs are intensified under high load levels, elevated temperatures, and humid environments. A predictive capability on the overall nonlinear viscoelastic response of the FMLs that recognizes different responses in the FRP and metallic layers becomes necessary. Literature indicates a few advances in this direction by the consideration of the elastic-plastic behavior and the use of classical lamination theory (Chen & Sun, 1989; Hashagen et al., 1995). Pindera et al. (1989) have carried out an experimental investigation of the creep response of ARALL laminates at 121°C. A pronounced viscoelastic behavior is observed in ARALL at stress levels below its proportional limit. Aluminum exhibits a nonlinear viscoelastic behavior while aramid-FRP shows a linear viscoelastic behavior. The classical lamination theory (CLT) was used to model the overall creep response of the laminates.
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Giles, Andrew, and Satchi Venkataraman. "Characterization of Interlaminar Fracture Energy for Asymmetric Laminates With Residual Thermal Strains." In ASME 2023 Aerospace Structures, Structural Dynamics, and Materials Conference. American Society of Mechanical Engineers, 2023. http://dx.doi.org/10.1115/ssdm2023-107076.

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Abstract Hybrid composite laminates or fiber metal laminates (FML’s) with fiber reinforced polymer (FRP) matrix composites reinforced with metal foils have been investigated for improvements in fatigue, impact resistance and bearing strengths. In this study, to measure fracture properties of interface of metal foil with FRP composite lamina, the specimens with laminate layup [012, AF, |SS, AF, 012] were used; where 0 represents a 0-degree IM7/977-3 unidirectional pre preg ply, AF represents 3M™ AF-191 adhesive film, and SS represents a 0.005 inch 304 full hardened stainless-steel layer. The location of the starter crack obtained using a Teflon insert is indicated by “|”. Although the full laminate is symmetric, the two adherents on either side of the crack plane are not. Further, the presence of the metal (Stainless steel foil) on the surface of one of the adherents leads to warping of the adherents due to the mismatch in the thermal expansion coefficients and asymmetry of the lay-up of the adherent sub-laminates. This paper discusses a method for accounting for composite laminate asymmetry, residual thermal stresses, and various contact conditions over a crack surface to obtain fracture toughness. MATLAB program was developed to determine the necessary equations and calculation steps required for processing fracture toughness, as well as for automating the data reduction process. Utilizing these new calculation methods, estimations of GIIc values from test data with and without thermal corrections for two different adhesive thicknesses were obtained. A comparison showed the corrected method led to 8% to 20% higher GIIc values.
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Okumuş, F., and A. Turgut. "Thermal Behavior of Aluminum Metal-Matrix Composite During Cooling Process." In ASME 2001 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. American Society of Mechanical Engineers, 2001. http://dx.doi.org/10.1115/detc2001/rsafp-21744.

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Abstract The paper presents a thermal behavior analysis of metal matrix composite lamina and laminates during a cooling process. A long stainless steel fiber reinforced aluminum metal matrix composite lamina and laminate are used for this purpose. Metal matrix composites were manufactured by using modulus under the action of 30 MPa pressure and heating up to 600 °C. The thermal stresses generated during cooling have a profound effect on the distortion and strength of the composite materials. In this study, thermal stresses, residual stresses and effective thermal expansion coefficients as a function of orientation angle of the aluminum metal matrix composite during a cooling process are investigated. The finite element method was used for thermal stress analysis. For this purpose, four noded rectangular elements were used in the ANSYS finite element code.
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N, Vasiraja, Vasanthanathan A PhD, and Sathishkumar D. "Finite Element Analysis of Glass Fibre Reinforced-Fibre Metal Laminate Composite with Different Stacking Arrangements." In International Conference on Advances in Design, Materials, Manufacturing and Surface Engineering for Mobility. SAE International, 2020. http://dx.doi.org/10.4271/2020-28-0382.

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Hahn, Marlon, Christian Weddeling, Nooman Ben Khalifa, and Arash Shabaninejad. "Springback Behavior of Carbon-Fiber-Reinforced Plastic Laminates With Metal Cover Layers in V-Die Bending." In ASME 2016 11th International Manufacturing Science and Engineering Conference. American Society of Mechanical Engineers, 2016. http://dx.doi.org/10.1115/msec2016-8532.

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The V-die bending of a carbon-fiber reinforced thermoplastic laminate bonded to thin cover layers made of microalloyed steel was investigated. Such hybrid semi-finished products are gaining importance in transport-related lightweight designs. Experiments were conducted for different forming temperatures and dwell times to determine suitable process parameters. The punch radius was varied to evaluate its influence on the springback/negative springback of the fiber-metal laminate (FML). The results, which are in good accordance with a simple analytical model, showed that the solidification of the composite core can compensate for the springback of the metal layers. Micrographs further revealed that the fiber orientation can affect the thickness distribution in the bend area.
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Ball, D. L., and W. S. Chan. "A Constitutive Model for Distributed Microcracking in Titanium Matrix Composite Laminae." In ASME 1999 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1999. http://dx.doi.org/10.1115/imece1999-0518.

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Abstract The ply constitutive relations of an energy-based model for distributed microcracking in continuous fiber reinforced metal matrix composites are presented. Simple models for damage progression are used in conjunction with these damage dependent constitutive relations to allow the prediction of fatigue life under constant amplitude, isothermal conditions. The microcracking model is discussed in the context of fatigue analysis of unnotched titanium matrix composite laminates. Analytical results generated by using this model in a unidirectional laminate analysis algorithm are presented and compared with experimental results.
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Riddle, Robert A., Donald R. Lesuer, and Chol K. Syn. "Damage Initiation and Propagation in Metal Laminates." In ASME 1996 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1996. http://dx.doi.org/10.1115/imece1996-0157.

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Abstract The metal laminates proposed here for use in aircraft structures consist of aluminum alloy interlayers between aluminum alloy based metal matrix composite (MMC) plates reinforced with silicon carbide particles. The properties of the laminates are to be tailored for applications in jet engine fan containment and in various wing and auxiliary support structures. One important mechanical property of the metal laminate is fracture toughness. This composite metal structure is designed to have enhanced ductile fracture properties as a result of the plastic formability of the aluminum layers and increased strength and stiffness due to the layers of the metal matrix composite. The enhanced fracture properties of the metal laminates are measured by fracture toughness specimens of several designs. Of particular interest is the optimum thickness of the ductile interlayer to optimize the fracture properties, but have the least effect on the strength and the stiffness. Specimen designs have been chosen which should allow measured properties of the specimen deformation and failure to be translated into predictions of component strength in actual aerospace applications. One mode of crack growth which increases fracture toughness and damage resistance in applications of interest is extensive delamination between the ductile interlayer and the MMC plates. The total area of delamination is increased by the tendency of metal laminates to have damage initiate at the lobes of contours of effective plastic strain which are significantly off-axis from the plane of Mode I or tensile mode opening crack growth. This off-axis damage increases the delaminated area and is a factor in forcing the crack to reinitiate at a new location in the next MMC plate. Experimental evidence for this phenomena is presented, along with finite element calculations which quantify and explain enhanced fracture values. The progressive damage is modeled using tie-break slidelines with critical strains to failure chosen with the help of elastic-plastic fracture mechanics calculations.
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Wu, Haoyu, Zhiwei Chen, Fang Ji, Xiaoliang Jia, and Jinhui Wang. "A Review: The Effect of Laminate Parameters on the Performance of Fibre-Reinforced Composite Pressure Vessel." In ASME 2024 Pressure Vessels & Piping Conference. American Society of Mechanical Engineers, 2024. http://dx.doi.org/10.1115/pvp2024-123544.

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Abstract Sustainable development has become the main theme of the world’s economic development nowadays. Hydrogen energy, as a new type of clean energy, has received extensive attention and focused research from countries in recent years, and the search for safe, efficient, economical and more energy-saving hydrogen storage technologies is the main direction of hydrogen energy utilization development. With the increasing requirements for the light weighting of hydrogen storage pressure vessels and the growing maturity of composite material design and processing technologies, various pressure vessels have evolved from metal tanks to fiber-reinforced pressure vessels (FRPVs) over the past decade or so, mainly to reduce weight and increase pressure ratings. Fiber-wound pressure vessels are an important direction for the future development of high-pressure vessels, and during the preparation of fiber-reinforced pressure vessels, the parameters of the winding and molding process play a crucial role in the performance of the products. In this paper, the effects of design and process parameters such as resin mass fraction, fiber volume fraction, winding tension, winding path, winding pattern, etc. on the forming process of FRPV winding layer and the performance and quality of the finished products are reviewed, and different optimization techniques for each parameter are summarized, and the problems and development trends are proposed to provide a reference for the research on the forming process of fiber-wound pressure vessels.
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